-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-23-00-860-001 29-23-00-860-002 Disconnection of the Isolation Coupling of the Power Transfer Unit (PTU)Connection of the Isolation Coupling of the Power Transfer Unit (PTU)
3. Job Set-up__________
Subtask 29-10-00-860-066
A. Aircraft Maintenance Configuration
(1) Make sure that the aircraft is in this configuration: - the spoilers 1 thru 5 retracted, - all servo controls in their neutral positions.
(2) Disconnect the isolation coupling of the Power Transfer Unit (PTU) (Ref. TASK 29-23-00-860-001).
4. Procedure_________
Subtask 29-10-00-220-050
A. Do this Functional Test for the Green Hydraulic System
R R R (1) Use a ground service cart with a FLOWMETER 20 L.MN (5.2833 US GAL.MN), calibrated to +/- 1.5% over full range to pressurize the Green hydraulic system (Ref. TASK 29-10-00-863-001).
(2) Make a record of the flow rate.
R (3) Make sure that the flow rate is not more than 9 l (2.3775 USgal)/minute.
(4) If the flow rate is too high, do the full check of internal leakage to find the cause (Ref. TASK 29-00-00-280-001) (Ref. TASK 29-00-00-280-004).
(5) Depressurize the Green hydraulic system (Ref. TASK 29-10-00-864-001).
Subtask 29-10-00-220-052
B. Do this Functional Test for the Yellow Hydraulic System
R R R (1) Use a ground service cart with a FLOWMETER 20 L.MN (5.2833 US GAL.MN), calibrated to +/- 1.5% over full range to pressurize the Yellow hydraulic system (Ref. TASK 29-10-00-863-002).
(2) Make a record of the flow rate.
R (3) Make sure that the flow rate is not more than 10 l (2.6416 USgal)/minute.
(4) If the flow rate is too high, do the full check of internal leakage to find the cause (Ref. TASK 29-00-00-280-003) (Ref. TASK 29-00-00-280-004).
(5) Depressurize the Yellow hydraulic system (Ref. TASK 29-10-00-864-002).
5. Close-up________
Subtask 29-10-00-860-067
A. Put the aircraft back to the serviceable condition.
(1) Remove the ground service cart and the flow meter from the aircraft.
(2) Connect the isolation coupling of the Power Transfer Unit (PTU) (Ref. TASK 29-23-00-860-002).
TASK 29-10-00-220-002
Functional Check to Monitor Internal Leak Rate of Blue Hydraulic System
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1.
Reason for the Job
__________________
Refer to the MPD TASK: 291900-02
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific FLOWMETER 20 L.MN (5.2833 US GAL.MN), calibrated to R +/- 1.5% over full range
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-00-00-280-002 Check of the Internal Leakage of the Blue Hydraulic System 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM HYDRAULIC POWER 液壓1(122)
